Supersonic speed large maneuvering target continuous large overload maneuvering height stability control method
A stable control method and large maneuvering technology, applied in the direction of adaptive control, general control system, control/regulation system, etc., to achieve the effect of simple and reliable working mode
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[0038] In order to make the object, technical solution and advantages of the present invention clearer, refer to the attached figure 1 -3 The present invention is described further.
[0039] The invented roll angle instruction online planning method comprises the following steps:
[0040] Step 1: Solve the required overload for altitude stability control
[0041] The highly stable control adopts the classic control theory PD control structure, and its structure diagram is as follows: image 3 As shown, the stable altitude needs to use the overload command
[0042] no Hc =k vy [k H (H c -H)-V y ] (8)
[0043] In the formula, H c Indicates the height command of the target flight, H is the current height of the target, V y is the component of the velocity of the target on the y-axis of the emission system, k H 、kvy is the height control parameter of the target, n Hc The overload command in the y-axis direction of the launch system required for altitude maintenance.
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